N306PQ
Registered owner: DELTA AIR LINES INC, GA (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
52 reports on file, 2014-08-31 – 2024-04-11.
Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 21,511 hrs · 16,210 cycles
L/H COCKPIT FLOOR BEAM IS CRACKED IN LOWER O/B FWD RADIUS AT FS 280 REPAIRED LEFT COCKPIT FLOOR BEAM AT LBL12 IAW MHIRJ REO 690-53-11-1716 REV-- DATED 2024-04-08
Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 21,511 hrs · 16,210 cycles
R/H COCKPIT FLOOR BEAM IS CRACKED IN LOWER O/B FWD RADIUS AT FS 280 REPAIRED RIGHT COCKPIT FLOOR BEAM AT RBL12 IAW MHIRJ REO 690-53-11-1716 REV-- DATED 2024-04-08
Part: DRAG ANGLE — DEFORMED (ZONE 800) · airframe 21,511 hrs · 16,210 cycles
AFTER REMOVAL OF PAX DOOR DRAG ANGLE FOUND HOLES ON WEB COMMON TO BE ENLARGE AND FOUND 1EA DOUBLE DRILL HOLE. REPAIRED IAW ENDEAVOR AIR EA CRJ952-16330 REV-A DATED 4/5/2024.
Part: LUG — DEFORMED (ZONE 600) · airframe 21,511 hrs · 16,210 cycles
"FOUND BOTH LUGS LABELED ""C"" & ""F"" ON THE R/H AILERON ARE PREVIOUSLY OVERSIZED. FABRICATION OF O/S BUSHINGS (QTY. 2) IS REQUIRED. REPAIRED IAW BOMBARDIER REO 670-57-61-237 REV-- DATE 2017-07-25. "
Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 21,511 hrs · 16,210 cycles
PAX DOOR AFT DRAG ANGLE IS CRACKED. INSTALLED PAX DOOR AFT DRAG ANGLE WITH PN 601R311772-5 IAW CRJ900 SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01, 51-42-22-001-001-A01 AND 51-42-15-001-001-A01.
Part: CROSSBEAM — CORRODED (BS 280) · airframe 21,511 hrs · 16,210 cycles
R/H FS280 CROSSBEAM CORRODED BETWEEN BL0 AND RBL 11. REPAIRED R/H FS280 CROSSBEAM CORRODED BETWEEN BL0 AND RBL 11 IN ACCORDANCE WITH MHIRJ REO 690-53-11-1717 DATE 2024-03-29 REV (--). SEE SHEET 2 FOR DTI REQUIREMENTS
Part: ATTACH FITTING — CORRODED (ZONE 200) · airframe 21,511 hrs · 16,210 cycles
CORROSION FOUND ON GALLEY ATTACHMENT FITTING BETWEEN FS 280-295 AT RBL 27. GALLEY MOUNTING BRACKET AT RBL 27 F.S. 280 - F.S. 295 IS IDENTIFIED AS P/N SH670-32149-3 AND HAS CORROSION PRESENT BOTH AROUND AND INSIDE OF BOLT HOLE AND IS FOUND TO BE OUT OF LIMITS IAW CRJ-900 SRM 53-21-43-101-001-A03. PART REQUIRES REPLACEMENT. REMOVED FITTING AT FS 280 - FS295 RBL 27 IAW CRJ 900 SRM 51-42-21-001-001-A01. LOCATED AND DRILLED NEW BRACKET (P/N: SH670-32149-3) IAW CRJ900 SRM 51-40-11-001-001-A01. INSTALLED NEW BRACKET (P/N: SH670-32149-3) IAW CRJ900 SRM 51-42-06-001-001-A01.
Part: FITTING — CORRODED (GALLEY) · airframe 21,511 hrs · 16,210 cycles
CORROSION FOUND ON GALLEY ATTACHMENT FITTING BETWEEN FS 280-295 AT RBL 18. GALLEY MOUNTING BRACKET AT RBL 18 F.S. 280 - F.S. 295 IS IDENTIFIED AS P/N SH670-32149-3 AND HAS CORROSION PRESENT BOTH AROUND AND INSIDE OF BOLT HOLE AND IS FOUND TO BE OUT OF LIMITS IAW CRJ-900 SRM 53-21-43-101-001-A03. PART REQUIRES REPLACEMENT. INSTALLED NEW BRACKET (P/N: SH670-32149-3) IAW CRJ900 SRM 51-42-06-001-001-A01.
Part: LUG — DEFORMED (ZONE 500) · airframe 21,511 hrs · 16,210 cycles
"FOUND BOTH LUGS LABELED ""C"" & ""F"" ON THE L/H AILERON ARE PREVIOUSLY OVERSIZED. FABRICATION OF O/S BUSHINGS (QTY. 2) IS REQUIRED. REPAIRED IAW BOMBARDIER REO 670-57-61-237 REV-- DATE 2017-07-25. "
Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 21,511 hrs · 16,210 cycles
FS 280 FWD J-ANGLE IS CORRODED INSTALLED J-ANGLE PN: CC670-34095-1 AT FS 280 BETWEEN RBL 11 TO LBL 11 IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
Part: BRACKET — CRACKED (EMERGENCY EXIT) · airframe 21,511 hrs · 16,210 cycles
L/H AFT EMERGENCY EXIT DOOR UPPER FWD DOOR ALIGNMENT BRACKET IS CRACKED AT BASE OF BRACKET, REPAIRED LH AFT EMERGENCY EXIT DOOR UPPER FWD DOOR ALIGNMENT BRACKET BY COMPLYING WITH ENDEAVOR AIR EA CRJ952-16264 REV IR DATED 4 APR 2024
Part: LUG — CRACKED (EMERGENCY EXIT) · airframe 21,511 hrs · 16,210 cycles
L/H FWD EMERGENCY EXIT DOOR FORMER CRACKED AT UPPER ALIGNMENT LUG. REPAIRED LH FWD EMERGENCY EXIT DOOR UPPER ALIGNMENT LUG BY COMPLYING WITH ENDEAVOR AIR EA CRJ952-16265 REV IR DATED 4 APR 2024
Part: LUG — CRACKED (EMERGENCY EXIT) · airframe 21,511 hrs · 16,210 cycles
RH FWD EMERGENCY EXIT DOOR FORMER CRACKED AT UPPER ALIGNMENT LUG REPAIRED BY COMPLYING WITH ENDEAVOR AIR EA CRJ952-16266 REV IR DATED 4 APR 2024
Part: ENGINE — FLUCTUATES (LEFT) · airframe 21,126 hrs · 15,885 cycles
WHILE CLIMBING OUT OF ORF THROUGH 13,000' PILOT HEARD A LOUD NOISE. LH ENG N1 WAS FLUCTUATING BETWEEN 30%-60% AND RUNNING ROUGH. FOLLOWED SEVERE ENGINE DAMAGE CHECKLIST AND SHUT DOWN LH ENG. AIRCRAFT CURRENTLY AOS WITH ENGINE CHANGE.
Earlier reports · 2014–2023 · 38 reports
2023
Part: PSEU — NONE · airframe 19,192 hrs · 14,219 cycles
LEVELED OFF AT FL250 AT 290 KTS. HEARD A NOISE IN THE NOSE GEAR BAY ALONG WITH A SLIGHT SHUDDER, FOLLOWED BY A GEAR DISAGREE WARNING. NOISE AND SHUDDER REOCCURRED AS WARNING EXTINGUISHED. INSUFFICIENT TIME BEFORE WARNING EXTINGUISHED TO PERFORM QRH ITEMS. REMOVED AND REPLACED PSEU PER AMM 32-61-01. PERFORMED POWER UP TEST OF LANDING GEAR PSS PER AMM 32-61-00, TEST PASSED. JACKED AND PERFORMED EXTENSION/RETRACTION OF THE LANDING GEAR SYSTEM IAW CRJ 900 AMM 32-30-00. PERFORMED SEVERAL SWINGS, NO ISSUES NOTED, ALL GEARS UP AND LOCKED. PERFORMED OVERSPEED INSPECTION OF LANDING GEAR PER JC 900-05-900-911. NO FINDINGS.
2020
Part: CHANNEL — GOUGED (VERTICAL STAB) · airframe 15,010 hrs · 10,714 cycles
VERTICAL STAB LEADING EDGE, PUNCTURE ON CHANNEL 1.5 INCH, MARKED WITH ORANGE TAPE. FABRICATED CHANNEL, IAW CRJ 900 SRM 51-24-21-001-001-A01 REV 38 DATED 72-25-20 AND SRM 51-24-36-001-001-A01 AND 51-40-11-001-001-A01 AND INSTALLED PER SRM 51-42-06-001-001-A01.
Part: HINGE — DAMAGED (RUDDER) · airframe 15,010 hrs · 10,714 cycles
RUDDER CENTER HINGE BEARINGS 2 EA HAVE EXCESSIVE PLAY. FOUND BOTH CENTER HINGE FITTINGS TO HAVE BORE DAMAGE. REMOVED, DRILLED UP, & INSTALLED 2 EA HINGE FITTINGS P/N: AV67021081-015 & AV67021081- 013, IAW CRJ 900 SRM 51-40-11-001-001-A01 & 51-42-21-001-001-A01.
Part: HINGE — DAMAGED (RUDDER) · airframe 15,010 hrs · 10,714 cycles
RUDDER CENTER HINGE BEARINGS 2 EA HAVE EXCESSIVE PLAY. FOUND BOTH CENTER HINGE FITTINGS TO HAVE BORE DAMAGE. REMOVED, DRILLED UP, & INSTALLED 2 EA HINGE FITTINGS P/N: AV67021081-015 & AV67021081-013, IAW CRJ 900 SRM 51-40-11-001-001-A01 & 51-42-21-001-001-A01.
Part: ANGLE — CORRODED (FUSELAGE) · airframe 15,010 hrs · 10,714 cycles
FS 280 FWD J-ANGLE IS CORRODED. MAINTENANCE PERFORMED CORRECTIVE ACTION NR 1, IAW CRJ 900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.
Part: DOOR SILL — CORRODED (AFT CARGO) · airframe 15,010 hrs · 10,714 cycles
AFT BAGGAGE BAY DOOR CUTOUT LOWER THRESHOLD CORROSION INDICATIONS FS 1020 TO FS 1045, FOUR PLACES AS MARKED. REMOVED & REPLACED AFT CARGO DOOR SILL P/N MM670-35655-003, IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, 51-42-21-001-001-A01, 51-40-11-001-001-A01, 51-41-02-001-001-A01. LEAK CHECK GOOD.
Part: DOOR FRAME — CORRODED (BS 280) · airframe 15,010 hrs · 10,714 cycles
FS 280.00 BULKHEAD, LT DOOR FRAME SKIN IS CORRODED AT FLOOR LEVEL. REPAIRED FS 280.00 BULKHEAD LT DOOR FRAME SKIN, IAW REO 670-53-11-745 REV-A DATED 2016/10/28.
Part: BRACKET — CORRODED (FWD CARGO) · airframe 15,010 hrs · 10,714 cycles
FWD CARGO BAY BRACKET IS CORRODED BETWEEN FS 565 TO FS 580 AT STGR 27. LOCATED AND INSTALLED BRACKET PN SH670-33389-2 AT FS 565-580 STRINGER 27, IAW CRJ 900 SRM 51-42-21-001-001-A01 AND IAW CRJ 900 SRM 51-42-22- 001-001-A01.
Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 15,010 hrs · 10,714 cycles
PAX DOOR SURROUND STRUCTURE HAS CORROSION ON MID FLOOR SUPPORT ANGLE. REMOVED AND REPLACED ANGLE, IAW CRJ 900 SRM 51-42-06-001-A01.
Part: ANGLE — CORRODED (SRVCE DOOR SILL) · airframe 15,010 hrs · 10,714 cycles
CORROSION FOUND ACROSS SERVICE DOOR LOWER SILL. REMOVED & REPLACED SERVICE DOOR LOWER SILL P/N: SH670-31996-3, IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-21-001-001-A01.
Part: ANGLE — CORRODED (PAX DOOR SILL) · airframe 15,010 hrs · 10,714 cycles
PAX DOOR SURROUND STRUCTURE HAS CORROSION ON SILL ANGLE. REMOVED AND REPLACED PAX DOOR SILL ANGLE, IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
2019
Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 13,598 hrs · 9,613 cycles
PAX DOOR EXTERNAL EMERGENCY LIGHT LENS IS CRACKED. REMOVED AND REPLACED PAX DOOR EMERGENCY LIGHT LENS IAW AMM 33-51-15.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 12,769 hrs · 8,958 cycles
DURING PRE FLIGHT INSPECTION EMERGENCY EXIT LIGHTING ON THE LOWER SIDE WALL AT ROW 13 FOUND TO BE INOP ON BOTH SIDES. REPLACED BATTERY PACK (EMERGENCYLIGHTS) AT PS 38 IAW CRJ 900 AMM 33-51-17 OPS TEST GOOD THIS CLEARS MEL MM02 UPDATED PLACARD REMOVED MOC NOTIFIED #95909
2018
Part: OXYGEN MASK — NO TEST (FIRST OFFICER'S) · airframe 10,936 hrs · 7,619 cycles
FIRST OFFICER`S OXYGEN MASK WILL NOT SHUT OFF DURING TEST. R & R THE OXYGEN MASK IAW AMM 35-11-12. OPS CHECKED NORMAL.
Part: FLASHLIGHT — INOPERATIVE (MAIN CABIN) · airframe 10,867 hrs · 7,566 cycles
FA FLASHLIGHT NOT CHARGING, NO CHARGE LIGHT SHOWN. REPLACED THE FLASHLIGH BATTERY IAW AMM
2017
Part: OXYGEN MASK — UNWANTED DEPLOY (JUMP SEAT) · airframe 8,709 hrs · 6,010 cycles
OXYGEN MASK ON FA JUMPSEAT DEPLOYED AFTER LANDING. STOWED THE FLT ATTENDANT OXYGEN MASK IAW AMM 35-11-12. OK FOR SERVICE
Part: SEAL — BROKEN (PBE) · airframe 8,643 hrs · 5,960 cycles
RED SEAL ON PBE IN COCKPIT BROKEN. INSTALLED THE SEAL IAW AMM 35-31-06.
Part: UNKNOWN — ODOR (CABIN) · airframe 8,366 hrs · 5,754 cycles
ODOR OF AN OVERHEATING MOTOR WITH RECIRCULATION FAN ON, GOES AWAY WITH FAN OFF. PULLED AND COLARD CIRCUIT BREAKER 1 A5 , 2 A5. RAN RECIRCULATION FANS FOR TWO HOURS AND PERFORMED OPERERATIONAL TEST IAW AMM 21-22-10. ALL CHECKED GOOD NO ODOR NOTED AT THIS TIME. ALL MIX PROCEDURES COMPLIED WITH MOC53430.
Part: FAN — INOPERATIVE (CABIN) · airframe 7,770 hrs · 5,311 cycles
BOTH FA'S REPORTED HEAVY ELECTRICAL ODOR IN FWD PART OF CABIN BETWEEN ROW1 AND FA JUMPSEAT. OVEN NOT IN USE. NO SMOKE OBSERVED. ACCOMPLISHED + INSPECTED AREA FOR SMELL PER FIM 21-22-00. ISOLATED SMELL COMING FROM LEFT PACK. DEFERRED LEFT PACK PER MEL 21-51-1B. NO HISTORY LAST 30 DAYS FOR SMELL IN CABIN. LT PACK PACK OPS CK'D GOOD IAW AMM 21-51-00 NO B1 CODES NOTED FOR LT PACK TROUBLESHOT TO GALLEY EXHAUST FAN LOW SPEED. R&R GALLEEY/LAV FAN IAW AMM 21-23-93 OPS CK GOOD REMOVED AND REPLACED LT RECIRC FILTER IAW J/C 900-21-180-701.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 7,585 hrs · 5,170 cycles
STR 27 HAS CORROSION SPOTS BETWEEN FRAMES 319.70 TO JUST FWD OF FRAME 310, IN THE FWD E & E BAY. OUT OF LIMITS. REPAIRED STR 27 IAW EA CRJ953-05486 REV IR.
Part: CHANNEL — CRACKED (E&E BAY) · airframe 7,585 hrs · 5,170 cycles
DIAPHRAM JUST TO THE RIGHT OF STGR 27 HAS CORROSION BETWEEN FRAMES 364 AND 349, IN THE FWD E&E BAY. REMOVED AND REPLACED DIAPHRAM RIGHT OF STGR 27, FR 364-FR 349 IAW SRM 51-42-06 + 51-42-21 OPS TEST OF THE MAIN AVIONICS DOOR IS GOOD IAW AMM 52-42-00-710-801.
Part: HANDLE — CRACKED (E&E DOOR) · airframe 7,585 hrs · 5,170 cycles
MAIN AVINICS COMPT. DOOR OUTER HANDLE IS CRACKED. REMOVED AND REPLACED AVIONICS DOOR HANDLE IAW AMM 52-42-02. OPS TEST OF THE MAIN AVIONICS DOOR GOOD IAW AMM 52-42-00-710-801.
Part: CHANNEL — CORRODED (FUSELAGE) · airframe 7,585 hrs · 5,170 cycles
(OK TO INSTALL TCAS CHANNEL) STGR27 CORRODED AT FS295. REMOVED AND REPLACED STRINGER AND RESTORED FINISH IAW SRM 51-42-06, 51-42-21 AND 51-25-16.
Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 7,585 hrs · 5,170 cycles
MAIN ENTRY DOOR AFT DRAG ANGLE IS CRACKED. REPAIRED ENTRY DOOR AFT DRAG BRACE ANGLE IAW REO 670-52-11-072.
Part: CHANNEL — CRACKED (FAIRING) · airframe 7,585 hrs · 5,170 cycles
AFT WING TO BODY FAIRING SPLICE CHANNEL IS CRACKED. REMOVED CRACKED CHANNEL ON AFT WING TO BODY FAIRING, AND REPLACED W/NEW SERV CHANNEL IAW SRM 51-42-13.
Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 7,585 hrs · 5,170 cycles
LT 280 CROSSBEAM IS CORRODED OUT OF LIMITS. REMOVED AND REPLACED WITH NEW BEAM PER SRM 51-42-06, 51-42-13 AND 51-42-21.
Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 7,585 hrs · 5,170 cycles
RT 280 CROSSBEAM IS CORRODED. REMOVED AND REPLACED WITH NEW BEAM PER SRM 51-42-06, 51-42-13 AND 51-42-21.
Part: DIAPHRAGM — CORRODED (FUSELAGE) · airframe 7,585 hrs · 5,170 cycles
DIAPHRAM JUST TO THE LEFT OF STGR 27 HAS CORROSION ON BOTH SIDES BETWEEN FRAMES 364 AND 349, IN THE FWD E & E BAY. OUT OF LIMITS. REMOVED AND REPLACED DIAPHRAM LEFT OF STGR 27 FR 364- FR 349 IAW SRM 51-42-06 + 51-42-21.
Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 7,585 hrs · 5,170 cycles
RT FLOOR SILL AT FS 280 HAS CORROSION AT THE TOP AND BOTTOM SIDE IN CABIN. OUT OF LIMITS. CUT OUT DAMAGE AND REPAIRED PER SRM 53-21-43.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 7,585 hrs · 5,170 cycles
FWD ANGLE SIDE OF 280 BEAM HAS CORROSION BETWEEN LBL 12 AND RBL 12, IN FLT DECK BELOW FLOOR. REMOVED AND REPLACED WITH NEW FLOOR SUPPORT PER SRM 51-42-06.
2016
Part: PBE — UNSERVICEABLE (COCKPIT) · airframe 5,907 hrs · 4,019 cycles
COCKPIT PBE VACUUM SEAL BROKEN. INSTALLED SERVICEABLE PBE IAW AMM 35-31-06.
2015
Part: UNKNOWN — ODOR (COCKPIT & CABIN) · airframe 3,219 hrs · 2,146 cycles
WITH APU ON & BOTH PACKS ON ENS OFF, INSTANT SMELL OF SMOLDERING PLASTIC & RUBBER. MOSTLY IN FLIGHT DECK BUT THROUGHOUT ACFT. NO FAULTS FOR ANY ASSOCIATED SYSTEMS NOTED IN MDC. INSPECTED AFT EQUIP BAY, NO DISCREPANCIES NOTED. PERFORMED APU BLEED AIR OPS CHECK WITH LT & RT PACKS. UNABLE TO DUPLICATE DISCREPANCY. COMPLETED PACK BURN PROCEDURE TO REMOVE ANY RESIDUAL CONTAMINATION FROM DUCTING. ALL CHECKED GOOD, ALL WORK IAW AMM 21-51-00. RESEALED AFT EQUIP BAY IAW GMM 8.13.
Part: ESCAPE HATCH — OUT OF ADJUST (COCKPIT) · airframe 2,724 hrs · 1,786 cycles
CREW HATCH LEAKING AT RT CORNER LOWER PART OF HATCH. INSPECTED FITS & CLEARANCES OF CREW ESCAPE HATCH AS WELL AS SEAL & HATCH LOCKING PINS & RECEPTACLES FOR SECURITY. FOUND HATCH TO BE OUT OF ADJUSTMENT & RIG LE DOWN MORE THAN .070"". SEAL OKAY IAW MM 52-22-00.
Part: SEAL — LACK OF LUBE (ESCAPE HATCH) · airframe 2,573 hrs · 1,685 cycles
CREW ESCAPE HATCH LEAKING WATER. LUBRICATED THE CREW ESCAPE HATCH SEAL IAW AMM 12-20-52 PARA 4 STEP A 3.
2014
Part: LIGHT — UNSECURE (CABIN) · airframe 2,112 hrs · 1,395 cycles
EMERGENCY FLOOR PATH LIGHTING UNSECURE IN FWD GALLEY, LT SIDE & DIRECTLY BEHIND FWD LAVATORY ON RT SIDE. SECURED EMER FLOOR PATH IAW AMM 33-51-01.
Part: LIGHT — UNSECURE (CABIN) · airframe 1,655 hrs · 1,103 cycles
FLOOR STRIP IN FRONT OF GALLEY CART B CAME UP IN FLIGHT. SECURED EMER FLOOR STRIP IAW AMM 33-51-01. NO OTHER DEFECTS NOTED AT THIS TIME.
Part: SKIN — DENTED (FUSELAGE) · airframe 1,353 hrs · 900 cycles
MAINTENANCE IS TASKED WITH PERMANENT REPAIR OF A DENTS IN THE LT FUSELAGE SKIN BETWEEN FS 1000.00 & FS 1015.00, STRINGER 20L & 21L. THE DENTS MEASURE 4.00 X 2.50 X .002 DEEP & 5.60 X 3.10 X .015 DEEP. REPAIRED IAW EA CRJ953-2883.
Part: SEAL — BROKEN (PBE) · airframe 1,361 hrs · 903 cycles
PBE SECURITY SEAL BROKEN FLIGHT DECK. R & R PBE SECURITY IAW AMM 20-00-00.